CN107963232A - One kind ejection aircraft and its system - Google Patents
One kind ejection aircraft and its system Download PDFInfo
- Publication number
- CN107963232A CN107963232A CN201711296240.0A CN201711296240A CN107963232A CN 107963232 A CN107963232 A CN 107963232A CN 201711296240 A CN201711296240 A CN 201711296240A CN 107963232 A CN107963232 A CN 107963232A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- borded pile
- aircraft body
- propeller
- ejection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000000034 method Methods 0.000 claims abstract description 4
- 238000005507 spraying Methods 0.000 claims abstract description 4
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/14—Attitude, flight direction, or altitude control by jet reaction the jets being other than main propulsion jets
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
One kind ejection aircraft and its system, belong to aircraft field, including aircraft body, borded pile and gag lever post.Aircraft body includes flywheel, screw-casing, propeller, high voltage gas cabin and valve.The ejection aircraft and its system work process：Aircraft body is sleeved on borded pile, is inflated using external high pressure equipment from valve for high voltage gas cabin, high-tension apparatus is removed after inflation, open valve, the reaction force of spraying high-pressure gas will promote aircraft body to be moved along borded pile, so as to drive screw-casing, affect propeller works.After aircraft body departs from borded pile, due to the presence of flywheel, propeller will be rotated further, and be glided in the air for aircraft body and be provided a power.A kind of ejection aircraft and its system of the present invention, principle is simple, simple in structure, takes off for fixed wing aircraft model and provides a platform, reduces the requirement to place, and can realize that airplane catapult is started to walk, and glides over long distances in the air, without power.
Description
Technical field
One kind ejection aircraft and its system, belong to aircraft field, more particularly to a kind of aircraft and its system.
Background technology
Traditional fixed wing aircraft model either takes off still to circle in the air in the air and is required for using motor either gasoline engine
As power；And fixed wing aircraft model take off it is higher to site requirements, it is necessary to the runway of long enough distance, it is impossible to
When take off everywhere.
The content of the invention
The present invention program is in order to for insufficient existing for such scheme, a kind of ejection aircraft of invention and its system.
One kind ejection aircraft and its system, including aircraft body, borded pile and gag lever post.Aircraft body include flywheel,
Screw-casing, propeller, high voltage gas cabin and valve.
The borded pile perpendicular fastener is on a tablet.The gag lever post perpendicular fastener in the tablet where borded pile
On, by borded pile side.The screw-casing is connected with propeller.The propeller is placed in aircraft body front end.The flywheel with
Propeller is connected.The high voltage gas cabin is placed in aircraft body, and high voltage gas cabin both ends axle center is threaded a pipe.The valve is placed in aircraft
Body tail section, connects high voltage gas cabin.
Preferably, the aircraft body is consistent with conventional fixed-wing aircraft shape.
Preferably, the gag lever post is placed in borded pile side, and left and right one, symmetrical, function is identical.
Preferably, the valve can air inlet can also deflate.
The ejection aircraft and its system work process：Aircraft body is sleeved on borded pile, is set using external high pressure
It is standby to be inflated from valve for high voltage gas cabin, high-tension apparatus is removed after inflation, opens valve, the reaction force of spraying high-pressure gas
Aircraft body will be promoted to be moved along borded pile, so as to drive screw-casing, affect propeller works.Aircraft body departs from borded pile
Afterwards, since the presence of flywheel, propeller will be rotated further, glide in the air for aircraft body and a power is provided.
A kind of ejection aircraft and its system of the present invention, principle is simple, simple in structure, takes off for fixed wing aircraft model
One platform is provided, reduces the requirement to place, and can realize that airplane catapult is started to walk, is glided over long distances in the air, without dynamic
Power.
Brief description of the drawings
Fig. 1 is ejection aircraft and its system schematic；Fig. 2 is ejection aircraft schematic diagram；Fig. 3 is in ejection aircraft
Portion's structure diagram.
In figure, 1- aircraft bodies, 2- borded piles, 3- gag lever posts, 11- flywheels, 12- screw-casings, 13- propellers, 14- high pressures
Gas cabin, 15- valves.
Embodiment
The present invention is illustrated in conjunction with attached drawing, one kind ejection aircraft and its system, including aircraft body 1,
Borded pile 2 and gag lever post 3.Aircraft body 1 includes flywheel 11, screw-casing 12, propeller 13, high voltage gas cabin 14 and valve 15.
2 perpendicular fastener of borded pile is on a tablet.3 perpendicular fastener of gag lever post is in flat with the place of borded pile 2
On plate, by 2 side of borded pile；Left and right one, symmetrical, function is identical.The screw-casing 12 is connected with propeller 13.It is described
Propeller 13 is placed in 1 front end of aircraft body.The flywheel 11 is connected with propeller 13.The high voltage gas cabin 14 is placed in aircraft body
In 1,14 both ends axle center of high voltage gas cabin is threaded a pipe.The valve 15 is placed in 1 afterbody of aircraft body, connects high voltage gas cabin 14.It is described
Valve 15 can air inlet can also deflate.The aircraft body 1 is consistent with conventional fixed-wing aircraft shape.
The ejection aircraft and its system work process：Aircraft body 1 is sleeved on borded pile 2, utilizes external high pressure
Equipment is inflated from valve 15 for high voltage gas cabin 14, and high-tension apparatus is removed after inflation, opens valve 15, spraying high-pressure gas
Reaction force will promote aircraft body 1 to be moved along borded pile 2, so as to drive screw-casing 12, affect propeller 13 to work.Aircraft sheet
After body 1 departs from borded pile 2, due to the presence of flywheel 11, propeller 13 will be rotated further, and be glided and be carried in the air for aircraft body 1
For a power.
Claims (5)
1. one kind ejection aircraft and its system, it is characterised in that：Aircraft body（1）, borded pile（2）And gag lever post（3）；Aircraft
Body（1）Including flywheel（11）, screw-casing（12）, propeller（13）, high voltage gas cabin（14）And valve（15）；The borded pile
（2）Perpendicular fastener is on a tablet；The gag lever post（3）Perpendicular fastener in borded pile（2）On the tablet at place, by borded pile
（2）Side；The screw-casing（12）With propeller（13）It is connected；The propeller（13）It is placed in aircraft body（1）Front end；It is described
Flywheel（11）With propeller（13）It is connected；The high voltage gas cabin（14）It is placed in aircraft body（1）It is interior, high voltage gas cabin（14）Two end axles
The heart is threaded a pipe；The valve（15）It is placed in aircraft body（1）Afterbody, connects high voltage gas cabin（14）.
2. a kind of ejection aircraft according to claim 1 and its system, it is characterised in that：It is described ejection aircraft and its
System work process：By aircraft body（1）It is sleeved on borded pile（2）On, using external high pressure equipment from valve（15）For high pressure gas
Cabin（14）Inflation, removes high-tension apparatus after inflation, open valve（15）, the reaction force of spraying high-pressure gas, which will promote, to fly
Machine body（1）Along borded pile（2）Movement, so as to drive screw-casing（12）, affect propeller（13）Work；Aircraft body（1）It is de-
From borded pile（2）Afterwards, due to flywheel（11）Presence, propeller（13）It will be rotated further, and be aircraft body（1）Glide in the air
One power is provided.
3. a kind of ejection aircraft according to claim 1 or 2 and its system, it is characterised in that：The gag lever post（3）Put
In borded pile（2）Side, left and right it is each one or more.
4. a kind of ejection aircraft according to claim 1 or 2 and its system, it is characterised in that：The borded pile（2）With
Gag lever post（3）It can also be arranged to certain gradient.
5. a kind of ejection aircraft according to claim 1 or 2 and its system, it is characterised in that：The valve（15）I.e.
Energy air inlet can also deflate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711296240.0A CN107963232A (en) | 2017-12-08 | 2017-12-08 | One kind ejection aircraft and its system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711296240.0A CN107963232A (en) | 2017-12-08 | 2017-12-08 | One kind ejection aircraft and its system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107963232A true CN107963232A (en) | 2018-04-27 |
Family
ID=61998436
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711296240.0A Withdrawn CN107963232A (en) | 2017-12-08 | 2017-12-08 | One kind ejection aircraft and its system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107963232A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110857146A (en) * | 2018-08-24 | 2020-03-03 | 北京理工大学 | Carry on many rotor unmanned aerial vehicle's delivery system |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2598607Y (en) * | 2002-12-31 | 2004-01-14 | 刘建鑫 | Simple direct-rising model aircraft |
| US20050178895A1 (en) * | 2003-01-17 | 2005-08-18 | Mcgeer Brian T. | Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion |
| CN101327846A (en) * | 2008-06-13 | 2008-12-24 | 北京航空航天大学 | Small-sized unmanned aerial vehicle rotating ejector rack |
| CN102120496A (en) * | 2010-10-22 | 2011-07-13 | 王先全 | Vacuum power catapult |
| CN105667789A (en) * | 2016-01-13 | 2016-06-15 | 中国科学院自动化研究所 | Universal type elastic potential energy mechanical catapult for single tandem wing unmanned aerial vehicle with rear propeller |
| CN106742027A (en) * | 2017-01-16 | 2017-05-31 | 方桂平 | Aircraft steam ejection device and its method of work |
| CN106853872A (en) * | 2015-12-08 | 2017-06-16 | 熵零股份有限公司 | A kind of aircraft catapult method and its system |
| CN206434864U (en) * | 2017-02-09 | 2017-08-25 | 薛泽厚 | A kind of aircraft of VTOL |
-
2017
- 2017-12-08 CN CN201711296240.0A patent/CN107963232A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2598607Y (en) * | 2002-12-31 | 2004-01-14 | 刘建鑫 | Simple direct-rising model aircraft |
| US20050178895A1 (en) * | 2003-01-17 | 2005-08-18 | Mcgeer Brian T. | Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion |
| CN101327846A (en) * | 2008-06-13 | 2008-12-24 | 北京航空航天大学 | Small-sized unmanned aerial vehicle rotating ejector rack |
| CN102120496A (en) * | 2010-10-22 | 2011-07-13 | 王先全 | Vacuum power catapult |
| CN106853872A (en) * | 2015-12-08 | 2017-06-16 | 熵零股份有限公司 | A kind of aircraft catapult method and its system |
| CN105667789A (en) * | 2016-01-13 | 2016-06-15 | 中国科学院自动化研究所 | Universal type elastic potential energy mechanical catapult for single tandem wing unmanned aerial vehicle with rear propeller |
| CN106742027A (en) * | 2017-01-16 | 2017-05-31 | 方桂平 | Aircraft steam ejection device and its method of work |
| CN206434864U (en) * | 2017-02-09 | 2017-08-25 | 薛泽厚 | A kind of aircraft of VTOL |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110857146A (en) * | 2018-08-24 | 2020-03-03 | 北京理工大学 | Carry on many rotor unmanned aerial vehicle's delivery system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180427 |
|
| WW01 | Invention patent application withdrawn after publication |